Wireless signaling system



Feb. 13, 1951 F. c. WILLIAMS 2,541,627

WIRELESS SIGNALING SYSTEM Filed July 25. 1947 3 Sheets-Sheet l LgTRANSMITTER 0' TO I I C F3 |2 RECEIVER M GENTR A.V. C.

FIG. I.

Lusec GONIOMETER H IO PULSE AND COURSE I eeN INDICATOR RECEIVER \l5 Invento I4 c. mums I -c Attorney Feb. 13, 1951 I c, w u s 2,541,627

WIRELESS SIGNALING SYSTEM ZERO OF PHASE THROUGH NORTH.

Inven for F. 0. William Attorney Feb. 13, 1951 F. c. WILLIAMS 2,541,627

WIRELESS SIGNALING SYSTEM Fil ed July'25, 1947 v a Sheets-Sheet s Fig. 5

B ELECTRONIC swITcI-I 5 TRANSMITTER L RELAY J R C M C coNTRnI M L oscILLAToR D N B S DELAY (BUFFER STAGE REcEIvER TRANSMITTER fjl ELECTRONIC swITcI-I 5 J 1 3 DELAY I 4 A.V.C. l 1 SEC.

REFERENCE 2O PHASE UNIT L\- PULSE GENERATOR GONIOMETERT 2| lBEARINs WAVEFORM L l GENERATOR PHASE COMPARATOR Attorney Patented Feb. 13, i951 UNITED STATES PATENT OFFICE Application July 25, 1947, Serial No. 763,712 In Great Britain May 24, 1945 Section 1, Public Law 690, August 8, 1946 Patent expireslviay 24, 1965 proved arrangements by which the navigator of r such a mobile craft may obtain useful information regarding his bearing with respect to a known geographical position and, with certain and preferred embodiments thereof, may also be provided with an indication of the amount and direction of deviation with respect .to a chosen course line towards or away from such known position.

-' The scope of the invention is defined in the appended claims. ofit, information is provided in a mobile craft as to its bearing direction with respect to a known geographical position by the comparison of the phase relationship of a first alternating current or voltage derived from the reception of pulse signals radiated repeatedly in cyclic order from each of a plurality of aerials spaced about the known position with respect to a second or reference alternating current'or voltage whose frequency is the same as that of the cyclic repetition of the ground transmissions and whose phase is related to the cyclic order timing of the radiations from each of said spaced aerials.

- The first alternating current or voltage is derived from the cyclic variation of the transit time required for signals to reach the mobile craft from each of the fixed aerials in turn due to their spacing.

The second reference alternating voltage or current is conveniently provided by the transmission of a suitably modulated signal from a further aerial located at the centre of said spaced aerials. This modulated signal may comprise a series of pulse signals at the same recurrence frequency as those from the spaced aerials and occurring at af'fixed timing relationship therewith, said further pulse signals being width-modulated in synchronism with the cyclic .order of transmission from said'spaced aerials. e .In a convenient constructional arrangement four spaced aerials are provided located one at eachflcorner of a square and fed in turn with groups of pulses from one transmitter through a rotary switch: A further aerial located at the ntre of the square'is fed with pulses from a "second transmitter, said pulses being width modulated insinusoidal fashion in synchronism with the rotation of the switch controlling the supply pf pulses to saidspaced aerials.

In the preferred embodiment I 21 Claims. (01. 343-105) In order that the above and further features of the invention may be more readily understood embodiments thereof will now be described,by way of example only, with referenceto the ac'-'-' companying drawings in which:

Figure 1 is a diagram showing the layout of a fixed ground or beacon transmitting station constructed in accordance with the invention.

, Figure 2 is a block schematic diagram of the apparatus provided in the mobile craft for use in conjunction with the ground station of Fig.1; while Figures 3 and 4 are waveform diagrams illus trating the operation of the arrangement shown in Figure 2. 1 I

Figure 5 illustrates in block schematic form one modified form of ground beacon transmitter while Figure 6 shows an appropriately modified mobile craft arrangement adapted for use with the beacon of Figure 5,

Figure 7 is a schematic block diagram of a simplified beacon arrangement.

Referrin to Figure 1, T and To indicate two pulse transmitters operating respectively ondifferent frequencies f and T0 of the order, of, say 200 mc/s. It will be assumed for convenience of description that the transmitters are both located at O in the centre of the square A, B, C, D, and that the line AC lies in the north-south direction although such a lay-out is not essential to the successful operation of the arrangement.

Transmitter T is modulated at a pulse-recurrence frequency of, say, 5 kc/s. and its output is supplied by way of a four-quadrant switch S, also located at the point 0, to one or other of-four aerials located respectively at the corners A, B, C and D of the square. The switch S is rotated v times per second so that, assuming perfect switching, each aerial at A, B, C or D will radiate groups of 25 pulses in turn, such groups being recurrent at 50 C. P. S. Transmitter To is also modulated at the same pulse recurrence frequency, e. g., 5-kc/s., as transinstant in the rotation cycle of the switch S, e .fg.,

regarded as located at a point P so distant fromG that lines joining O, A, B, C and D to P may be considered to be parallel, then certain simple relations will exist for the time-*di-fierence which will occur between the reception at the mobile craft of a pulse radiated from aerial O and the corresponding pulse radiated from one of the aerials A, B, C, or D.

For instance, if the distance via a direct "transmission line from transmitter T at point to any one of the aerialsat..A, B, C =or:D':*a an'd'a pulse has a velocity "v in such transmission-line then the time difference tA for the'aerial A\(i. e., time via aerial A- time direct from aerial 0 will equal where eds the'velocity of em. waves in'air and (his the bearing angle of the point .P with reference to the line through A and'Cie, due north. Similarly if 133, tC and tD are the time difierences for aerialsB, C and D then Referring now to :EigureZ, which illustrates in 'blockschematic form the appara'tusarrangement in the :mobilecraf-t, affirstlreceiver 10 connected te -aerial H and tuned to frequency of transmitter T provides a :pulse waveform output .from the ;pulse signals received :from the corner aerials A E, C and- D. Asecond and similar receiver l2 connected to aerial l-3 -and tune'd to frequencyifo of transmitter Tn.provides a-ipulse waveform out put from the :pulse signals received from the centre aerial :0.

The pulse waveform output from receiver 10,

in addition to operating an A. V. 0. system M 01 the receiver 10, is also applied to a pulse generating unit H: which provides a .lmicro-second .pulse commencing in coincidence with the leading edge of each received pulse. This 1 micro-second pulse waveform'output is applied to abearing waveform unit 46 whose function'and construction will be dealt with later.

The output waveform from receiver 1 2 "is similarly used to operate an-A. V. C. system H for the receiver I2 and to control a second .pulse generating unit 18 which provides 1 micro-sec- 0nd -pulses, each commencing in coincidence with the leading edge of each pulse received from the centre aerial O. This :1 micro-second pulse wave- 'form is also applied to the bearing waveform unit 16.

By suitable choice of value for the-distance .a previously referred to'between transmitter T-and each of the aerials :A,'B,-C,ID, the above described 1 micro-second pulses may be made 'to overlap 'one another within 'the unit [6, the degree of overlap, being variable in accordance with change in the aforesaid time-difference factor. In view of the possible positive or negative value of the sine or cosine term in the time-difierence expressions previously evolved it is desirable so to arrange the overlap that, when no sine or 00- sine term is present (i. e., when '0 equals either 0, or 270), it is 0.5 micro-second and for this purpose an artificial delay it may be introduced at the transmitter T to make this overlap time i. e.,

The maximum time-difierence change due to the sine or cosine terms is a/c and this is made equal to-O.2'5 micro-second thereby leaving 0.25 microsecond of overlap as tolerance at either end of the range of overlap variation. With such choice of values the dimensionzz becomes approximately 250 'feet.

Figure 3-.(-a') illustrates rat 30,.a l micro-second pulse derived from a :pulse signal :from centre aerial O and at 31 asimilar 1 micro-second pulse derived from the corresponding signal from a corner aerial when 0 is such that the sine or cosine term of the previously-quoted expressions disappears and when %+.t= 0.5 .micro-second It will 'be-seen that the leading edgeof the corner aerial'pulse is coincident in time with :the midpoint of the centre aerial pulse. This condition may be defined as the 'zero or mean condition of -overlap-so that the smear cosine terms when present introduce positive or negative outputs according to whether the degree of overlap increases or decreases.

Figure 3-(21 illustrates .a typical overlap condition when -0 .is such that a :sine -or cosine term is present. 30 indicates the centre aerial pulse as before While -32and 33 (indicate the corresponding pulses :from aerials at opposite corners e. g., A and C. The shaded portions illustrate the respective positive and negative overlaps about the above definedfzeroonmeaniconditi i'! Considering for the .moment :one corner aerial alone, e. g., the aerial atA, it will be recalled that groups of 25 .pulses are radiated therefrom 50 times per second. By the application of these, together with the corresponding pulses from the centre aerial O, .to'a'su'itable valve circuit, e. .g., .a gate valve arrangement, in thelbearing waveform unit 16 (Figure 2) itlis ,possible to derive, after suitable smoothing .a steady anode current in a valve which is proportionalto cos 0. 'IfTK is a constant of proportionality, '-K cos 0 may be said 'to represent the anode current for'ae'rial A. Similarly for 'ae'ria'ls'ByC and D "the anode current for thesame valve will'be, K 'sinB, "K cos 9 and K sin '6 giving an .anode current waveform as shown in Figure- 4(a). This waveform, of course, repeats itself 'a't150 C. P. 'S. and its-shape is a function of '0, i. e., is dependent "upon the bearing of the mobile craft with respect to the point 0 of the fixedground beacon.

The fundamental component df'this'wavef'orm can be shown to lag by the angle 0 on the reference sine wave of diagram Figure 4(b) which is obtained by suitable demodulation of the widthmodulated pulses received from transmitter To. The anode current waveform of Figure 4(a) may be resolved into two component waveforms as shown in Figure 4(c) and (d) due respectively to the signals from aerials A, C and B, D. Their fundamental components will be proportional to cos 0 and sin 0 respectively, the former leading the latter by 90. If the constant of proportionality equals K then, as shown in Figure 4(e) the fundamental component of the waveform of Figure 4(a), is e., that of the component waveforms of Figure 4(c) and 4(d) added together, lags behind the component K cos 0 by the angle 0. The component K cos 0 however is, by definition, in phase with the reference waveform of Figure 4(b) and the latter therefore leads by O on the said fundamental component of the bearing waveform.

It will be appreciated that the bearing of the a beacon from the aircraft, which is what is required, is not 0 but (1r0) (with the convention that angles east of north are positive and angles west of north are negative); this may readily be provided for by utilising, instead of the current waveform shown in Figure 4(a) the corresponding voltage waveform produced across a resistance in the anode circuit of the valve concerned.

Returning now to Figure 2, the resolved bearing waveform provided by the unit If is applied to a plied with the reference waveform of Figure 4(1)) derived, as already stated, from the width-modulated pulse signal output of receiver l2 through a reference phase unit 20 which serves to smooth the receiver output wave-form to one of sinusoidal form, and a goniometer or phase shifting device 2| by which any desired degree of phaseshift may be imparted to this reference waveform before its application to unit I!) for phase comparison with the output from unit is.

If the goniometer unit 2| is adjusted to impart a phase-shift equal to the angle 6 the phase comparison unit I9 provides an output which causes a centre-zero meter 22 to read zero on its associated scale 23. Any deviation of the angle 0 between the bearing and reference waveform will cause the meter 22 to swing to the left or right according to whether such deviation is one of lead or lag.

The goniometer unit 2| is adjusted by means of a control knob 24 throughla suitable linkage indicated diagrammatically at 25. The setting value of the goniometer unit is indicated, in terms of bearing angle (1r0) by the inter-connection of knob 2-! through a gear train 26 with a rotatable ring 2'! carrying a calibration in degrees cooperating with a fixed index mark 28.

By suitable calibration the meter 22 may be arranged to give a direct indication in degrees of any off-course deviation. The rotatable scale ring 21 conveniently surrounds the off-course meter as shown.

The various elements of both the ground beacon transmitting arrangement shown in Figure 1 and the mobile craft apparatus shown in Figure 2 may be of any suitable and well known form.

For example the transmitters T and T0 with their modulating arrangements may follow the constructions now well known in connection with radar and like pulse modulated equipment. The various aerials should, of course,ebe of the omni- 6? directional type. ofrotating brush form or alternatively of the rotating capacity type not making direct metallic contact between its stationary and-moving men1- hers.

I ii and I2 may again follow radar practice as may also the pulse generator units I5 and IS. The latter two units may conveniently comprise relaxation oscillator circuits of the so-called flipflop type, triggered to the unstable condition by each received pulse signal and reverting automatically to the stable condition after the chosen time interval of l micro-second. The bearing waveform unit l6, as already indicated, makes use of a gate valve circuit. This circuit may comprise a multi-electrode valve such as a pentode, normally held with its anode current out off by the application of suitable blocking potentials to both its control and its suppressor-grids. l micro-second pulse outputs from units l5 and 18 are of such value as separately to be incapable but in combination to be capable of opening up the valve so that, when both occur simultaneously, a set value of anode current flows for the precise period of theirsimultaneous occurrence or overlap. The unit 26 may comprise a suitable integrating network having a time-constant adapted to the switching frequency while the goniometer unit 2! may comprise a rotating coil or a rotating condenser form of goniometer device, the two opposite input elements of which are each supplied from the unit 20 through a suitable phase-splitting circuit. Several forms of such devices are shown, for example, in Termans Radio 'Engineers Handbook, 1943, at page 949. The phase comparison unit 19 may be of conventional'form adapted to provide an output whose magnitude and polarity are functions of the phase-relationship of ,the two applied input waveforms.

The use of two transmitting and two receiving channels is not essential. One alternative arrangement may comprise one transmitter which supplies pulses as before to the four corner aerialsmitter arrangement suitable for operation accord- Lil switch S under the control of a switching arrangement ES which may conveniently be of similar form to the spark-gap devices as used for common T and R working in certain forms of radar apparatus. The switching route provided by the device ES is controlled by an electronic relay control circuit RC which is normally stabilised in a condition by which the device ES routes the transmitter output to the rotary switch S but which may be momentarily tripped to an opposite condition by which the device ES routes the transmitter output to the centre aerial O. This momentary tripping is effected by an applied pulse waveform to the circuit RC.

The pulse modulating waveform for controlling the operation of the transmitter T is supplied by a unit M, which may conveniently comprise a stabilised oscillator circuit. This modulating waveform is applied directly to the modulating circuits MC of the transmitter T and also to a delay circuit DN by which a chosen time delay The rotating switch may be" In the mobile craft apparatus the receivers The 7 interval is. imposed. The delayed pulse output from this circuit DN is then applied as a tri gering input to. the relay control circuit RC and also, by way of a buffer stage BS, to the modulating circuit MC as a supplementary control input thereto.

In the operation of this beacon arrangement, each pulse of the original modulating waveform causes a first pulse to be generated by the transamitter T and applied by Way of the device E to the switch S and. thence to one f the co n aerials A, B, G. or D. After a delay interval et by t ircuit DN, he same pu e c uses the control circuit BC to chan e the device to its opposite condition and simultaneously effects a second pulsing of the transmitter T, .This second pulse. is radiat y Way f he c nt e aerial .O and, of course, carries the requisite Width modulation to provide the reference waveform at the mobile craft. The circuit RC and the device ES then revert to their original condition in readiness for the next pulse of the modulating waveform which causes a repetition of events.

In the mobile craft apparatus for this embodiment, shown in Figure 6, a single receiver IQ and its associated aerial Ii is used together with its A. V. C. system M. The receiver output is applied to an electronic switching circuit 31] by Which it may be directed either to a delay circuit 3| and thence to the l microesecond pulse generator circuit IE or to the other 1 micro-second pulse enerator circuit :8 and the associated reference phase unit 20. These units l5, [8 and 20 as well as the remaining elements leading to the indicator device are as already described in connection with Figures 24.

The switching circuit so may comprise a multivibrator type circuit having one stable and one unstable condition, the unstable condition being initiated by an applied input pulse which is arranged to be the first pulse of the related pair of beacon pulses. The unstable condition is dee signed to have a natural time duration only slightly larger than the delay time between the related pairs of beacon pulses so that the second of the related pair of pulses reverts the multivibrator circuit back to its stable condition.

In operation the second pulse of each related pair reverts the circuit back to its stable condition so that the first pulse of the next related pair of beacon pulses is directed to the delay circuit 35 and thence, as previously described, to units and It. The first pulse of each related pair triggers the circuit 3E into the unstable con dition so that the corresponding second pulse is directed to the units [8 and 2E! and thence again as previously described to units It, and E9. The delay imposed by the circuit 3.! is set so as to be precisely equal to that of the unit D of Figure 5 whereby the necessary overlap condition of the related pulses occurring in unit l5 may be obtained for operation in the manner already described in connection with the first embodiment.

The modulation of the transmitter To to pro-.- vide the reference waveform need not be sinusoi-. dal as described, it may be of pulsed, square-wave or other suitable form. Since such transmission is used purely as a convenient means of providing a reference waveform in the mobile craft, it may in some cases be dispensed with altogether and an oscillator or chronometer, capable of providing a waveform of sufficient frequency stability to remain accurately synchronised with the- 8 cyclic radiation f om the stated erials at the ground beacon, provided in its place- Alterna tively th pulses from thev transmit e T ma be width-modulated to provide the reference waveform. With su h latter ran em nt the seri s of pulses provided by the transmission from Tc for v rlap comp ri n rpo ay be re lac d by a phase-stable oscillator in the mobile craft;

said oscillator being synchronized by the received pulses radiated by the transmitter T,

The use of four corner aerials has been rig-1 scribed but three aerials or any number ex ceding.

in turn through transmission pathsv of equal length in similar manner to the system already described the zero-signal course line provided will;

be at right angles to the line joining the spaced aerials A, B, as shown at .r. The bearing wave,- form will be that shown in Figure 4(d) and as the angle 0 the changes sign the phase of the waveform will reverse and 0. to O. or 1r will de-.= This waveform is fed to aphasea fine the course. sensitive circuit which operates the centre-treading meter. No goniometer device is necessary,

An extension of this arrangement is to impose an additional delay time on the pulse signals sent:

to one of the two spaced aerials A or B. The

track or course line provided will then be a hyper.-

bola such as that shown at y in Figure 7..

A signalling channel from the beacon to the mobile craft e. g., for speech transmission, may

be provided by width modulation of the transmitted pulses from transmitter T or To or both." The 5 kcs. pulse-recurrence frequency and the 50' C. P. S. reference modulation frequency may be filtered out without loss of essential speech frequencies.

The use of pulse technique compared with the continuous-wave radiation as used in prior arrangements has the advantage of comparative immunity from fading. due with C. W. arrangements, to the interaction of waves reaching the mobile craft from .the transmitting aerials by the direct path and by one or more paths involving reflection from other objects. Since the one micro-second pulses used in the mobile craft with the present invention toi produce the bearing waveform are dependent for their formation on the first 0.25 micro-second,"

only of the received pulses, reflected pulses which arrive later than 0.25 micro-seconds behind the direct wave pulse will produce no adverse effect..

Since 0.25 micro-second is equal approximately to 250 feet of travel of e. in waves in air, the ground area over which detrimental reflection can take place is very limited. I claim:

1. In or for a navigation system for the guiding of a mobile craft such as an aircraft, a radio: beacon comprising a central aerial sited at the known location of said beacon, at least two other aerials spaced around said central aerial, means for feeding all said aerials with electromagnetic wave energy modulated with timing pulses at' the same repetition frequency, together with switching means for feeding said other aerials Such fading is normally in a'predetermined sequence wherebya continuous train of pairs of related pulses is radiated from the beacon and each related pair consists of a pulse radiated from said central aerial and a pulse radiated from one of said other aerials, the said other aerials being spaced around the central aerial in close proximity so that the time taken for an electromagnetic wave to traverse the distance between said central aerial and any one of said other aerials is such that in a receiver the pulses derived from'a related pair of said timing pulses overlap.

2 A radio beacon according to claim 1 wherein four said other aerials are provided equally spaced from said central aerial and located at each corner'of a square.

3. A radio beacon according to claim 1 and in which said switching means feed said other aerials in a cyclic sequence for equal periods.

4. In or for a navigation system for the guiding of a mobile craft such as an aircraft,- a radio beacon comprising afirst transmitter, a central aerial sited at the known location of said beacon and fed from said first transmitter with electromagnetic energy at a first carrier frequency modulat'ed with timing pulses at a constant repetition frequency, a second transmitter, at least two other aerials spaced around said central aerial and fed from said second transmitter with electromagnetic energy at a second carrier frequency modulated with timing pulses at said repetition frequency, together with switching means 'for feeding said other aerials in a predetermined sequence whereby a continuous train of pairs of related pulses is radiated from the beacon, each related pair consisting of a pulse radiated from said central aerial and a pulse radiated from one of said other aerials, the said other aerials being spaced around the central aerial in close proximity so that the time taken for an electromagnetic wave to traverse the distance between said central aerial and any one of said'other aerials is such that in a receiver the pulses derived from a related pair of said timing pulses overlap.

5. A radio beacon according to claim 4 in which four said other aerials are provided equally spaced from said central aerial and located at each corner of a square, said switching means feeds said four other aerials in a cyclic sequence for equal periods and in' which means are provided for width modulating the pulses radiating from said central aerial in synchronismwith the cyclic sequence of transmission from said other aerials.

6. In or for a navigation system for theguiding of a mobile craft such as an aircraft, a,radio beacon comprising a transmitter, a central aerial sited at the known location of, said beacon, at least two other aerials spaced around said central aerial, a first switching means whereby said transmitter feeds with electro-magnetic energy modulated with timing pulses at a constant frequency said central aerial and a second switching means for interlacing periods, said second switching means feeding said other aerials in a predetermined sequence so that a continuous train of pairs of related pulses is radiated fromthe beacon, each related pair consisting of a pulse radiated from said central aerial and a pulse radiated from one of said other aerials, the said other aerials being spaced around the central aerial in close proximity so that the time taken for an electromagnetic wave to traverse the distance between said central aerial and any one of said oth- "er aerials is such that in a receiver the pulses dc;-

10 rived from arelated pair of said timing pulses overlap.

7. A radio beacon according to claim 6 in which four said other aerials are provided equally spaced from said central aerial and located at each corner of a square and in which said second switching means feeds said four other aerials ina cyclic sequence for equal periods.

8. A radio beacon according to claim '7 and comprising modulating means to width-modulate and delay means to impose a predetermined delay on the pulses fed to said central aerial.

9. In or for a navigation system for the guiding of mobile craft such as an aircraft, a radio receiver for use in the mobile craft comprising 7 means for receiving a continuous train of pairs of related pulses, means for deriving for each received pulse a rectangular pulse of a constant width which is sufficient to make the pulses from each related pair overlap, and means for determining the degree of overlap of said related derived pulses.

10. In or for a navigation system for the guiding of a mobile craft such as an aircraft, a radio receiver for use in the mobile craft comprising means for receiving a continuous train of pairs of related timing pulses, each related pair of pulses consisting of a first pulse width modulated at a constant frequency and a second pulse, the interval between each pair of related pulses varying repetitively at the width modulation frequency, means for deriving from each received pulse a rectangular pulse of constant width which is sufiicient to make the pulses from each related pair overlap, means for producing output pulses said output pulses, and means for comparing the phase relationship between said first andsecond alternating currents.

11. In or for a navigation system for the guiding of a mobile craft such as an aircraft, a radio receiver for use in 'themobile craft comprising means for receiving a continuous train of pairs of related pulses at'the same carrier frequency, the interval between each relatedpair of pulses varying repetitively at a constant frequency and'the first pulse of each pair being width modulated at said constant frequency, delay means applied to the firstpulse of each related pulse which reduce the interval between each related pair of pulses, means for deriving from each received pulse a rectangular pulse of constant width, which is sufficient to make each related pair of pulses overlap, means for producing output pulses propor-' tional in magnitude to the degree of overlap of said related derived pulses, means for generating a first alternating current from the width modulation of said first pulses, means for generating a a 7s a, compl me tary-timingpulse for each pulse emitted from the first antenna, said last-named means including switching means for applying groups of such complementarypulses to said second and third antennas alternately, and a remote receiver whose position is to be ascertained, said receiver including means for efiecting a predetermined delay in the first pulse of each pair of complementary pulses, means responsive to the output of the last-named means for producing reformed complementary pulses, and means included in said receiver for measuring the respective overlaps of the reformed complementary pulses; said antennas being positioned in such close proximity and said pulses having so small an interval therebetween that the reformed complementary pulses will overlap.

13. In a beacon system, a receiver whose position is to be ascertained, a first antenna positioned at a known location, at least three other antennas symmetrically positioned about the first one, means for applying groups of pulses to the first antenna, means for applying complementary groups of pulses to one of the other antennas at a time, a switch to shift the output of the last- 'named means to each of the said other antennas in given sequence, said beacon system including means to cause signals resulting from com-plementary pulses to overlap, and said receiver ineluding means to indicate the durations of the respective overlaps.

14. In a navigation system, a first antenna at a predetermined location, second and third antennas located adjacent the first one and in different azimuthal directions therefrom, means for applying a pulse modulated radio frequency wave to the first antenna, means for producing a radio frequency wave having a complementary pulse modulation for each pulse of the first-named wave, said last-named means including switching means for applying the second radio frequency wave to said second and third antennas alternately at a repetition rate slower than the repetition rate of the pulses; and a remote receiver comprising means for'demodulating com complementary pairs of pulses, pulse generating means for deriving from each demodulated pulse a rectangular pulse of sufficient length to effect overlap of the derived pulses of each pair, and indicating means responsive to the overlap of said derived pulses.

15. In a beacon system, a receiver whose position is to be ascertained, a first antenna positioned at a known location, at least three other antennas symmetrically positioned about the first one, means for applying a radio frequency carrier to the first antenna and including modulating means for modulating said carrier with a series of pulses, means for generating a second radio frequency carrier and including modulating means for producing a complementary pulse for each pulse of the first-named series, means for repeatedly applying the second radio frequency carrier to said other aritennas'in a predetermined sequence, said beacon system including means to cause signals resulting from complementary pulses to overlap, and said receiver including means for giving indications depending on the overlaps of complementary pulses.

I6. 'In a navigation system, a firjst antenna at a predetermined location; second,third and fourth antennas located adjacent the first one and in different azimuthal directions therefrom; means for applying a first radio frequency carrier mod- 0nd radio frequency carrier having 911311156, complementary to each pulse of the first radio frequency carrier; said last-named means including switching means for repeatedly shifting the second radio frequency carrier to the second, third and fourth antennas in a particular sequence; signal-producing means associated with the switching means for producing a signal that varies according to the frequency at which the second carrier is shifted; and a remote receiver whose bearing is to be ascertained; said receiver including, a circuit for producing a current which varies according to the last-named signal, means for demodulating the first and second radio frequency carriers and producing a current that varies according to the difference in the time phase relationships of complementary pulses, and a phase-responsive measuring device comparing the phase relationship of said currents.

17. The system defined in claim 16 in which said radio frequency carriers have different radio frequencies, and in which the last-named means of claim 16 is responsive to approximately only the first quarter of a microsecond of a received pulse.

18. The system defined in claim '16 in which said signal producing means constitutes means for width-modulating the pulsesof the first radio frequency carrier at the frequency at which the second radio frequency carrier energizes the secondantenna, and in which said circuit is tuned to said shift frequency and produces an output current'of a frequency corresponding to the shift frequency.

19. An indicating device for use aboard a moving craft in conjunction with that form of navigation system in which there is a first width modulated pulsed carrier on one" frequency and a second carrier on'another frequency having pulse modulations complementary to those of the first carrier; means for demodulating the first carrier to produce a continuous train of width modulated pulses, means for generating a first alternating current of a frequency corresponding to the frequency of the width modulation of said first pulses, pulse generating means for deriving a rectangular pulse of a first predetermined length from each of said first'pulses; means for demodulating the second carrier to produce a continuous train of pulses, pulse generating means for deriving a rectangular pulse of a second predetermined length from each pulse of the last-named train of pulses, said first and second named pulse generating means both including means to elongate said rectangular pulses sufiiciently to cause complementary rectangular pulses to overlap in time, means for producing output pulses proportional in magnitude to the degree of overlap of the complementary rectangular pulses, said lastnamed means including agate controlled by the outputs of the first and second named pulse generating means for passing current when both of such outputs overlap in time, means responsive to said output pulses for generating a second alternating current in phase with the output pulses, and means for comparing the phase relationship of the first and second alternating currents and giving indications of such relationship.

20. A radio receiver for use in a navigation system of the type wherein two radio frequency carriers are pulsed at the same rate and emanate from known locations with the pulses of the first carrier being width-'modulated at a constant frequency comprising in combination, means for receiving and demodulating the first carrierto into an alternating current of a frequency the same as that of the Width-modulation, first pulse producing means for deriving a rectangular pulse of first predetermined length from each of the pulses of said demodulated output, means for demodulating the second carrier to produce a series of pulses, second pulse producing means for deriving a rectangular pulse of second predetermined length from each pulse of the last-named series, said first and second pulse producing means including means for suificiently elongating said rectangular pulses as to cause overlaps thereof when the two carriers have pulses that occur Within a predetermined time limit of each other, means for producing output pulses proportional in magnitude to the degree of overlap of the rectangular pulses derived from the two carriers, means for generating a second alternating current of a frequency depending on the frequency of said output pulses and in a predetermined phase relation with said output pulses, and means for comparing the phase relationship between said first and second alternating currents.

21. A radio receiver for use in a mobile craft comprising means for receiving a continuous train of pairs of related pulses at the same carrier frequency and of a form in which the interval between each related pair of pulses varies repetitively at a constant frequency and the first pulse of each pair being width'modulated at said constant frequency, an electronic switch for separating the first pulses in each related pair into a first channel and the second pulses in each related pair into a second channel, means in said first channel and responsive to said first pulses for producing a first alternating current at said constant frequency, a delay circuit in said first channel for delaying each first pulse, pulse pro- 14 ducing means in said first channel for deriving a rectangular pulse of a first predetermined length from each delayed first pulse, pulse producing means in said second channel for deriving a rectangular pulse of a second predetermined length from each received second pulse, said delay circuit and said first and second named pulse producing means having such constants that the rectangular pulses derived in said first channel will overlap time with the related rectangular pulse derived in said second channel when the pairs of related pulses reach the receiver within a predetermined time of each other, means for producing output pulses proportional in magnitude to the degree of overlap of said related rectangular pulses, means for procacing a second alternating current in phase with and derived from the magnitude variations of said output pulses, and indicating means for comparing the phase relationship between said first and second alternating currents.

FREDERIC CALL-AND WILLIAMS.

REFERENCES CITED The following references are of record in the file of this patent:

UNITED STATES PATENTS France June 30, 1924 

